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E-145 MEMORY ITEMS > Memory Items > Flashcards

Memory Items Flashcards

Memorize Memory Items

1
Q

02 MASK DONNING PROCEDURE

A 
HEADSET (REMOVE)
OXYGEN MASK (DON)
SMOKE GOGGLES if smoke present (ON)
REGULATOR if smoke/fumes present (EMER)
AFTER SMOKE PURGED (MASK 100%)
HEADSET (ON)
HOT MIC (OFF)
MASK MIC audio panel (MASK OUT)
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2
Q

SMOKE FIRE OR FUMES

A

OXYGEN MASKS - (DON 100%)
SMOKE GOGGLES - (DON)
CREW COMMUNICATION - (ESTABLISH)

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3
Q

SMOKE EVACUATION

A

OXYGEN MASKS - (DON 100%)
SMOKE GOGGLES - (DON)
CREW COMMUNICATION - (ESTABLISH)

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4
Q

BAGGAGE SMOKE

A

FIRE EXTG BAGG BUTTON (IF INSTALLED) -

PUSH IN

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5
Q

EFB FIRE CONCERNS

A

FLIGHT ATTENDANT - (EMER CALL)
GLOVES - DON
EFB AND MOUNT - RELEASE FROM WINDOW
EFB AND MOUNT - PURGE FROM COCKPIT

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6
Q

AILERON RUNAWAY/ROLL TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

AILERON SHUTOFF SYS 1 AND 2 - PUSH OUT

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7
Q

AIRPLANE OVERSPEED

A

AIRSPEED - MAX VMO/MMO

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8
Q

EMERGENCY DESCENT

A 
CABIN CREW - NOTIFY
FSTN BELTS - ON
THRUST LEVERS - IDLE
SPEED BRAKE - OPEN
AIRSPEED MAX - 250 KIAS
LANDING GEAR - DOWN
DESCENT - INITIATE
ALTITUDE - MEA OR 10,000 FT, WHICHEVER IS HIGHER
ATC - NOTIFY
IF UNABLE TO ESTABLISH COMMS - SQUAWK 7700
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9
Q

JAMMED AILERON

A

AILERON DISCONNECTION HANDLE - PRESS AND PULL

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10
Q

JAMMED ELEVATOR

A

ELEVATOR DISCONNECTION HANDLE - PRESS AND PULL

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11
Q

PITCH TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

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12
Q

RAPID CABIN DEPRESSURIZATION

A

CREW OXYGEN MASKS - DON

CREW COMMUNICATION - ESTABLISH

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13
Q

IF EMERGENCY DESCENT IS NECESSARY:

A 
CABIN CREW - NOTIFY
FSTN BELTS - ON
THRUST LEVERS - IDLE
SPEED BRAKE - OPEN
AIRSPEED MAX - 250 KIAS
LANDING GEAR - DOWN
DESCENT - INITIATE
ALTITUDE - MEA OR 10,000 FT, WHICHEVER IS HIGHER
ATC - NOTIFY
IF UNABLE TO ESTABLISH COMMS - SQUAWK 7700
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14
Q

ABNORMAL ENGINE START – TO ABORT START

A

ASSOCIATED THRUST LEVER - IDLE

ASSOCIATED START/STOP SELECTOR - STOP

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15
Q

RUDDER/YAW TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

RUDDER SHUTOFF SYS 1 AND 2 - PUSH OUT

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16
Q

APU FIRE

A

APU FUEL SHUTOFF VALVE - PUSH IN

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17
Q

BATTERY OVERTEMPERATURE

A

AFFECTED BATTERY - OFF

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18
Q

ATTCS FAILURE

A

THRUST LEVERS - MAX

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19
Q

DUAL ENGINE FAILURE

A

AIRSPEED - MIN 260 KIAS

OXYGEN MASK - AS REQUIRED

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20
Q

ENGINE FIRE, SEVERE DAMAGE, OR SEPARATION

A

ASSOCIATED THRUST LEVER - IDLE
ASSOCIATED START/STOP SELECTOR - STOP
ASSOCIATED FIRE EXTINGUISHING HANDLE - PULL (DO NOT ROTATE)

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21
Q

INADVERTENT SPOILER OPEN

A

SPEED BRAKE - CLOSE

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22
Q

STEERING SYSTEM INOPERATIVE OR
UNCOMMANDED SWERVING ON THE GROUND
– TAKEOFF OR LANDING

A

STEERING HANDWHEEL - DO NOT USE

STEERING DISENGAGEMENT BUTTON - PRESS

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23
Q

STABILIZED APPROACH CRITERIA – NOT GRADED

A

• From 1,000 feet
above the TDZE
FINAL LANDING CONFIGURATION SELECTED
ON GLIDE PATH WITH A SUSTAINED DESCENT RATE OF 1200 FPM OR
LESS
ON CORRECT LATERAL TRACK
ABOVE IDLE THRUST WITH AIRSPEED TRENDING TOWARDS CALCULATED
APPROACH SPEED PER SOP
• From 500 feet
above the TDZE
ABOVE IDLE THRUST AT CALCULATED APPROACH SPEED PER SOP (-5
KNOTS TO +10 KNOTS)
A minimum height for Vap not less than ___1,000___ feet above TDZE for approaches in IMC.
A minimum height for Vap not less than ___500_____ feet above TDZE for approaches in VMC.
If conditions are not met: A MISSED APPROACH MUST BE EXECUTED

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24
Q

MAXIMUM RAMP WEIGHT

A

XR - 53,351 LBS

LR - 50,044 LBS

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25
Q

MAXIMUM TAKEOFF WEIGHT

A

XR - 53,131 LBS

LR - 49,823 LBS

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26
Q

MAXIMUM LANDING WEIGHT

A

XR 44,092 LBS

LR 43,651 LBS

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27
Q

MAXIMUM ZERO FUEL WEIGHT

A

XR 40,785 LBS

LR 40,564 LBS

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28
Q

MINIMUM TOTAL AIR TEMPERATURE IN CRUISE

FLIGHT ABOVE 25,000 FT

A

-45 °C

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29
Q

NO MAINTENANCE ACTION IS REQUIRED IF

MOMENTARY DEVIATIONS OCCUR DOWN TO

A

-50°C

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30
Q

VLO FOR RETRACTION

A

200 KIAS

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31
Q

VLO FOR EXTENSION

A

250 KIAS

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32
Q

VLE

A

250 KIAS

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33
Q

VA

A

200 KIAS

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34
Q

MAXIMUM FLAP EXTENSION SPEEDS (XR)

A

9 – 250 KIAS
18 –200 KIAS
22 –180 KIAS
45 –160 KIAS

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35
Q

MAXIMUM FLAP EXTENSION SPEEDS ABOVE

10,000 FT AND Y/D DISENGAGED (XR Only)

A

9 - 250 KIAS
18 - 200 KIAS
22 - 180 KIAS
45 - 145 KIAS

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36
Q

MAXIMUM FLAP EXTENSION SPEEDS (LR)

A

9 – 250 KIAS
18 – 200 KIAS
22 – 200 KIAS
45 – (and momentarily) 145 (160 momentarily) KIAS

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37
Q

MAXIMUM ALTITUDE FOR FLAP EXTENSION

A

20,000 FT

38
Q

MAXIMUM TAKEOFF/LANDING TAILWIND

A

10 KTS

39
Q

MAXIMUM USABLE FUEL QUANTITY PER WING TANK

A

5,717 LBS

40
Q

UNUSABLE FUEL QUANTITY PER WING TANK

A

39 LBS

41
Q

MAXIMUM USABLE FUEL QUANTITY IN VENTRAL

TANK (XR)

A

1863 LBS

42
Q

UNUSABLE FUEL QUANTITY IN VENTRAL TANK

XR

A

21 LBS

43
Q

UNUSABLE FUEL QUANTITY WITH ANY

ASSOCIATED ELECTRIC PUMP INOPERATIVE

A

365 LBS

44
Q

MAXIMUM PERMITTED IMBALANCE BETWEEN TANKS

A

800 LBS

45
Q

MINIMUM FUEL TANK TEMPERATURE

A

-40 °C

46
Q

MAXIMUM FUEL TANK TEMPERATURE

A

52 °C

47
Q

APU MINIMUM TEMPERATURE

A

-54 °C

48
Q

APU MAXIMUM ALTITUDE FOR START

A

30,000 FT

49
Q

APU MAXIMUM OPERATIONAL ALTITUDE

A

37,000 FT

50
Q

APU MAXIMUM ROTOR SPEED

A

108%

51
Q

APU MAXIMUM ROTOR SPEED FOR AUTO

SHUTDOWN

A

104%

52
Q

APU MAXIMUM EGT FOR START

A

884 °C

53
Q

APU MAXIMUM EGT CONTINUOUS

A

680 °C

54
Q

APU EGT MAY BE EXCEEDED UP TO

A

717 °C FOR 5 MINUTES

55
Q

MINIMUM BATTERY TEMPERATURE FOR APU

START

A

-20 °C

56
Q

APU STARTER LIMITS

A

BETWEEN THREE CONSECUTIVE ATTEMPTS - 1 MINUTE OFF

BETWEEN 2 SETS OF 3 CONSECUTIVE ATTEMPTS 30 MINUTES OFF

57
Q

ENGINE MODEL

A

XR - AE3007A1E

LR - AE3007A1P

58
Q

N1 MAXIMUM

A

100%

59
Q

N2 MAXIMUM

A

XR - 105%

LR 102.4%

60
Q

ITT MAXIMUM FOR START

A

800 °C

61
Q

ITT MAXIMUM IN TAKEOFF MODES

A

XR - 970 °C FOR 5 MIN
XR – TEMPERATURES BETWEEN ___971__°C & __992___°C ARE TIME LIMITED TO __90____ SECONDS
LR - 948 °C FOR 5 MIN

62
Q

ITT MAXIMUM CONTINUOUS

A

XR - 935 °C

LR - 901 °C

63
Q

OIL PRESSURE BELOW 88% N2

A

MIN- 34 MAX- 110

64
Q

OIL PRESSURE AT OR ABOVE 88% N2 (XR)

A

MIN- 48 MAX- 110

65
Q

OIL PRESSURE AT OR ABOVE 88% N2 (LR)

A

MIN- 50 MAX- 110

66
Q

MINIMUM OIL TEMPERATURE

A

21 °C

67
Q

MAXIMUM OIL TEMPERATURE

A

126 °C

68
Q

MAXIMUM VIBRATION

A

HP- 1.1 LP- 1.8

69
Q

TAKEOFF THRUST MODES FOR TAKEOFF

A

XR (3 MODES) - E T/O, T/O, ALT T/O-1

LR (2 MODES) - T/O, ALT T/O-1

70
Q

ENGINE STARTER LIMITS – GROUND
STARTING OR DRY MOTORING
-OR THE FOLLOWING CYCLE LIMITS

A

UP TO 5 MINUTES ON, 5 MINUTES OFF

71
Q

ENGINE STARTER LIMITS – GROUND

FIRST TO FOURTH CYCLES

A

1 MINUTE ON, 1 MINUTE OFF

72
Q

ENGINE STARTER LIMITS – GROUND

FOLLOWING CYCLES

A

1 MINUTE ON, 5 MINUTES OFF

73
Q

ENGINE STARTER LIMITS – IN FLIGHT

MAXIMUM CONTINOUS OPERATION TIME

A

5 MINUTES ON

74
Q

ENGINE WARM UP – COLD ENGINE

A

4 MIN

75
Q

ENGINE WARM UP – WARM ENGINE

A

2 MIN

76
Q

ENGINE COOL DOWN

A

2 MIN

77
Q

MAXIMUM TEMPERATURE FOR ANTI-ICING OPERATIONS

A

10 °C

78
Q

MINIMUM TEMPERATURE FOR MANUAL ANTIICING OPERATION

A

-40 °C

79
Q

HOLDING CONFIGURATION

(GEAR, FLAPS, SPEED

A

GEAR UP, FLAPS UP, MIN 200 KIAS

80
Q

MAXIMUM AIRSPEED FOR WINDSHIELD WIPER

OPERATION

A

170 KIAS

81
Q

MAXIMUM LOAD ON MAIN GENERATOR

A

400 A

82
Q

MAXIMUM LOAD ON APU GENERATOR

UP TO FL300

A

400 A

83
Q

MAXIMUM LOAD ON APU GENERATOR

ABOVE FL300

A

300A

84
Q

MAXIMUM BATTERY TEMPERATURE

A

70 °C

85
Q

MAXIMUM DIFFERENTIAL PRESSURE

A

7.8 PSI

86
Q

MAXIMUM DIFFERENTIAL OVERPRESSURE

A

8.1 PSI

87
Q

MAXIMUM DIFFERENTIAL NEGATIVE PRESSURE

A

-0.3 PSI

88
Q

AUTOPILOT MINIMUM ENGAGEMENT HEIGHT

AFTER TAKEOFF

A

500 FT

89
Q

AUTOPILOT MINIMUM DECISION ALTITUDE

DURING ILS APPROACH

A

200 FT

90
Q

AUTOPILOT MINIMUM USE HEIGHT

XR

A

160 FT

91
Q

AUTOPILOT MINIMUM USE HEIGHT

LR

A

200 FT

92
Q

AUTOPILOT MALFUNCTION ALTITUDE LOSS

A

CRUISE 80 FT
MANEUVER 40 FT
ILS APPROACH 35 FT

E-145 MEMORY ITEMS (1 decks)

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